The invention discloses a blockade orbit optimization method based on a reachable domain, and belongs to the technical field of spaceflight. The method comprises the following steps: constructing a blockade time-varying reachable domain of a given orbit according to the initial state of a blockade and the mobility of the blockade; according to the time-varying reachable domain of the blocker for constructing the given orbit, the blocker intercepts the escape orbit in the reachable domain; and collecting the interception capability of the blockade for intercepting the escaped orbits in the reachable area, obtaining evaluation indexes, and obtaining an optimal blocked orbit. According to the method, the path for cutting off the escapes to the key area is formulated by analyzing the task execution ability of the blockade and the dominant area/dominant phase of the escapes.
本发明公开了一种基于可达域的封锁轨道优化方法,属于航天技术领域。方法包括根据封锁者的初态和封锁者的机动能力,构建给定轨道的封锁者时变可达域;根据构建给定轨道的封锁者时变可达域,使封锁者对可达域内的逃方轨道进行拦截;收集封锁者对可达域内的逃方轨道进行拦截的拦截能力,获取评价指标,得到最佳封锁轨道。本发明通过分析封锁者的任务执行能力,逃方的优势区域/优势相位,制定切断逃方通往关键区域的路径。
Reachable domain-based blockade orbit optimization method
一种基于可达域的封锁轨道优化方法
2024-11-22
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS / F41H Panzerung , ARMOUR / G06N COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS , Rechnersysteme, basierend auf spezifischen Rechenmodellen / G06Q Datenverarbeitungssysteme oder -verfahren, besonders angepasst an verwaltungstechnische, geschäftliche, finanzielle oder betriebswirtschaftliche Zwecke, sowie an geschäftsbezogene Überwachungs- oder Voraussagezwecke , DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTING PURPOSES |
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